On 3-D inelastic analysis methods for hot section components. Volume 1 : Special finite element models

Author:: Nakazawa, S.
Published:: May 1, 1988.
Physical Description:: 1 electronic document

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Summary:

This annual status report presents the results of work performed during the fourth year of the 3-D Inelastic Analysis Methods for Hot Section Components program (NASA Contract NAS3-23697). The objective of the program is to produce a series of new computer codes permitting more accurate and efficient 3-D analysis of selected hot section components, i.e., combustor liners, turbine blades and turbine vanes. The computer codes embody a progression of math models and are streamlined to take advantage of geometrical features, loading conditions, and forms of material response that distinguish each group of selected components. Volume 1 of this report discusses the special finite element models developed during the fourth year of the contract.

Other Subject(s):

STRUCTURAL MECHANICS

Collection:

NASA Technical Reports Server (NTRS) Collection.

Note:

Document ID: 19880012151.
Accession ID: 88N21535.
NAS 1.26:180893.
PWA-5940-62-VOL-1.
NASA-CR-180893.

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